Further Evaluation of Swept Wing Icing Scaling with Maximum Combined Cross Section Ice Shape Profiles
Author:
Affiliation:
1. Ohio Aerospace Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3183
Reference32 articles.
1. Current Experimental Basis for Modeling Ice Accretions on Swept Wings
2. Observations on the Growth of Roughness Elements into Icing Feathers
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